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    Hierarchical High-Fidelity Analysis Methodology for Buckling Critical Structures

    Source: Journal of Aerospace Engineering:;2005:;Volume ( 018 ):;issue: 003
    Author:
    Johann Arbocz
    ,
    James H. Starnes
    DOI: 10.1061/(ASCE)0893-1321(2005)18:3(168)
    Publisher: American Society of Civil Engineers
    Abstract: A hierarchical high-fidelity analysis methodology for predicting the critical buckling load of compression-loaded thin-walled isotropic shells is described. This hierarchical procedure includes three levels of fidelity for the analysis. Level 1 assumes that the buckling load can be predicted by the classical shell solution with simply supported boundary condition, and with a linear membrane prebuckling solution. Level 2 includes the effects of a nonlinear prebuckling solution and the effects of traditional clamped or simply supported boundary conditions. Level 3 includes the nonlinear interaction between nearly simultaneous buckling modes and the effects of boundary imperfections and general boundary conditions. Various deterministic and probabilistic approaches are used to account for the degrading effects of unavoidable shell-wall geometric imperfections. The results from the three solution levels are compared with experimental results, and the effects of the assumptions and approximations used for the three solution levels are discussed. This hierarchical analysis approach can be used in the design process to converge rapidly to an accurate prediction of the expected buckling load of a thin-shell design problem.
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      Hierarchical High-Fidelity Analysis Methodology for Buckling Critical Structures

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    https://yetl.yabesh.ir/yetl1/handle/yetl/45034
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    contributor authorJohann Arbocz
    contributor authorJames H. Starnes
    date accessioned2017-05-08T21:16:13Z
    date available2017-05-08T21:16:13Z
    date copyrightJuly 2005
    date issued2005
    identifier other%28asce%290893-1321%282005%2918%3A3%28168%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45034
    description abstractA hierarchical high-fidelity analysis methodology for predicting the critical buckling load of compression-loaded thin-walled isotropic shells is described. This hierarchical procedure includes three levels of fidelity for the analysis. Level 1 assumes that the buckling load can be predicted by the classical shell solution with simply supported boundary condition, and with a linear membrane prebuckling solution. Level 2 includes the effects of a nonlinear prebuckling solution and the effects of traditional clamped or simply supported boundary conditions. Level 3 includes the nonlinear interaction between nearly simultaneous buckling modes and the effects of boundary imperfections and general boundary conditions. Various deterministic and probabilistic approaches are used to account for the degrading effects of unavoidable shell-wall geometric imperfections. The results from the three solution levels are compared with experimental results, and the effects of the assumptions and approximations used for the three solution levels are discussed. This hierarchical analysis approach can be used in the design process to converge rapidly to an accurate prediction of the expected buckling load of a thin-shell design problem.
    publisherAmerican Society of Civil Engineers
    titleHierarchical High-Fidelity Analysis Methodology for Buckling Critical Structures
    typeJournal Paper
    journal volume18
    journal issue3
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(2005)18:3(168)
    treeJournal of Aerospace Engineering:;2005:;Volume ( 018 ):;issue: 003
    contenttypeFulltext
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